Precision Spacecraft Pointing Using Single-Gimbal Control Moment Gyroscopes with Disturbance
Author:
Affiliation:
1. Honeywell, Inc., Phoenix, Arizona 85382
2. Arizona State University, Tempe, Arizona 85287-6016
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4489
Reference20 articles.
1. Control synthesis for flexible space structures excited by persistent disturbances
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3. Steering law design for redundant single-gimbal control moment gyroscopes
4. Preferred gimbal angles for single gimbal control moment gyros
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